David L. Bacon
naca-tn-130
February, 1923
The airflow about a model while being tested is often sufficiently affected by the model support to lead to erroneous conclusions unless appropriate corrections are used. In this paper some new material on the subject is presented, together with a review of the airfoil support corrections used in several other laboratories.
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http://naca.central.cranfield.ac.uk/reports/1923/naca-tn-130.pdf